View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 00016U 58002A 24255.60796665 .00000799 00000-0 10633-2 0 9995
2 00016 34.2830 6.2647 2025942 282.7715 55.5188 10.49410356621295
| Epoch (UTC): | 11 September 2024 14:35:28 |
| Eccentricity: | 0.2025942 |
| inclination: | 34.2830° |
| perigee height: | 649 km |
| apogee height: | 4220 km |
| right ascension of ascending node: | 6.2647° |
| argument of perigee: | 282.7715° |
| revolutions per day: | 10.49410356 |
| mean anomaly at epoch: | 55.5188° |
| orbit number at epoch: | 62129 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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